Patent · US Active

Near synchronous distributed hydraulic motor driven actuation system

US10538310B2 · kind B2 · utility

5Cited by
6References
18Claims
0Family size

Assignee

Inventor

Key dates

Filing dateJun 5, 2017
Grant dateJan 21, 2020
Priority date
Expiry dateMar 8, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF15B2211/8757
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A control system may be used to control actuators that actuate movement of flight control surfaces of an aircraft. Each actuator is couplable to a flight control surface and includes a motion control assembly having a hydraulic motor and a drive path from the hydraulic motor to the flight control surface. Each hydraulic motor includes an extend port and a retract port. The system includes a hydraulic control module fluidly connected to the extend port and the retract port of each hydraulic motor and a controller operable to output hydraulic power from the hydraulic control module to the motion control assembly to actuate movement of the flight control surfaces. The controller is configured to identify an actuator that positionally leads the other actuators and reduce hydraulic power to the motion control assembly assigned to such actuator.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.